发明申请
US20090155051A1 DUPLEX TURBINE SHROUD 有权
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DUPLEX TURBINE SHROUD
摘要:
A gas turbine engine shroud includes a row of different first and second shroud segments alternating circumferentially therearound. The first segments have a first pattern of first cooling holes extending therethrough. The second segments have a second pattern of second cooling holes extending therethrough. The corresponding patterns have different collective flowrate capabilities.
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